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Most test pilot schools use multiple, more specific minimum control speeds, as V MC will change depending on the stage of flight. Other defined V MC s include minimum control speed on the ground (V MCG) and minimum control speed during approach and landing (V MCL).
Lift-off speed. [7] [9] V MC: Minimum control speed. The minimum speed at which the aircraft is still controllable with the critical engine inoperative. [7] Like the stall speed, there are several important variables that are used in this determination. Refer to the minimum control speed article for a thorough explanation.
The standards and certifications that specify airworthiness require that the manufacturer determine a minimum control speed (V MC) at which a pilot can retain control of the aircraft after failure of the critical engine, and publish this speed in the section of the airplane flight manual on limitations.
V mc a (Minimum control speed in the take-off configuration, a.k.a. air minimum control speed or minimum control speed in free air) see V speeds. The term and symbol are officially approved by the International Civil Aviation Organization (ICAO) and come from the French « vitesse minimale de contrôle en air libre ».
This allows the required data to be acquired in the minimum number of flight hours. The software used to control the flight test process is known as Flight Test Management Software, and supports the Flight Test Engineer in planning the test points to be flown as well as generating the required documentation. [citation needed]
Léon Lemartin, the world's first professional test pilot, [1] under contract to Louis Blériot in c. 1910 Jimmy Doolittle in 1928 with his Curtiss R3C-2, around the time he pioneered blind flying Chuck Yeager and the Bell X-1, first test pilot to break the sound barrier at Mach 1 in 1947 Neil Armstrong and the North American X-15 after a research test flight in 1960
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An important quantity in flying qualities measurements in turns or pull-ups is the variation of control force on the control stick or wheel with the value of acceleration normal to the flight direction expressed in g units. This quantity is usually called the force per g.